Abstract: A profile for a tool implementing a unified modeling language (UML) is described. The profile extends the UML to include decision management functionality. The profile includes stereotypes and customizations which generate question elements, decision elements, alternative elements, and the like. The association between the elements permits a design engineer to review previous decisions and the rationale behind the decisions. In particular, the one of alternative elements is associated with decision element by selected alternative relationship.

Abstract: A computer system records eye tracking data and identifies movements in the eye tracking data to determine gaze and pupil dynamics. Eye tracking data is correlated with a current task and predetermined vigilance requirements. The system determines if the user is exhibiting an appropriate level of vigilance based on the task or is becoming fixated. When fixation is detected, the system may engage in remedial action. A task flow diagram represents the operator tasks. Interactions between the user and the instrumentation are used to estimate the probability distribution of the task the user is currently conducting. The system correlates eye tracking data and physiological data such as electroencephalogram (EEG) and functional near-infrared spectroscopy (fNIRs) to determine neuroactivity. Monitoring neuroactivity reduces the probability of a false positive for fixation.

Abstract: A cabin management system is described. The cabin management system includes a housing. The housing is configured to receive one or more modules. The modules may be detached and reattached to the housing. The modules may be rearranged to achieve a desired layout of touchscreens, audio converter, and input/output ports. The modules may include a geometry which provides a flush-mounting between the housing and the modules. The flush-mounting may prevent a passenger from accessing the cavity defined by the housing. The audio converter includes a digital-to-analog converter and an audio jack. The digital-to-analog converter converts an uncompressed digital audio signal to an analog audio signal. The audio jack receives a stereo analog signal and outputs the stereo analog signal to an audio plug.

Abstract: A system for detecting an alignment of a relay lens assembly and a combiner of a head-up display is disclosed. The system includes an illuminated reticle spatially coupled to the relay lens assembly, an optical sensor spatially coupled to the combiner, and a control module configured to receive an input from the optical sensor, determine a position of the combiner relative to the relay lens assembly based on the received input; and generate an output based on a determined position of the combiner relative to the relay lens assembly. In another system, the illuminated reticle is spatially coupled to the combiner, and the optical sensor is spatially coupled to the relay lens assembly. The system may also participate in a feedback loop with the head-up display to reduce jitter in the head-up display.

Abstract: A runway overrun awareness and alerting system determines a breaking distance based on aircraft capabilities, and renders a graphical depiction of that breaking distance. The graphical depiction may be separately rendered on a head-up display and a primary flight display. The system may determine both a maximum deceleration breaking distance and a nominal deceleration breaking distance. The maximum deceleration breaking distance and nominal deceleration breaking distance may be separately rendered, and may be rendered to include a visual indicator if they exceed some safety threshold.

Abstract: The system may include at least one a light emitter configured to emit light over a range of wavelengths onto an environment and at least one sensor assembly. The range of wavelengths emitted by the light emitter may be of wavelengths that are above or below wavelengths used by a night vision imaging system. The sensor assembly may include an image sensor and conversion layer. The image sensor may capture images of the environment illuminated by the light emitters and sense light in a given range of wavelengths. The conversion layer may receive the emitted light and convert the emitted light to converted light with a wavelength within the given range of wavelengths associated with the image sensor. The image sensor may be further configured to receive the converted light from the conversion layer, capture an image of the light emitter and output image data associated with the captured image.

Abstract: A method and system for operating an ad hoc communication network under suboptimal commercial global navigation satellite system (GNSS) conditions and a loss of a base station communication link is disclosed. The method includes configuring the ad hoc communication network to operation in in-band or out-of-band mode, allowing device-to-device D2D communication. The method further includes configuring the ad hoc communication system to operate in overlay mode, sharing communication resources between network-controlled resources and D2D resources. The method further includes configuring the D2D resources with a base station precedent to the loss of the base station communication link and enabling the ad hoc communication network to operate in frequency hopping mode. The method further includes disabling physical sidelink control channel synchronization and/or resource management within the ad hoc communication network.

Abstract: A communication system is described. The communication system includes 5g base stations (gNodeB) which are communicatively coupled to a user equipment (UE) by a multiple radio access technology (multi-RAT) dual connectivity. A first of the gNodeBs is a master gNodeB which relays control signaling from a 5G network core to a secondary gNodeB. To avoid spectral interference of the control signals between the master gNodeB and the secondary gNodeB, the control signals are transmitted according to a tactical waveform protocol selected from the Department of Defense (DoD) Communication Waveform Inventory (2020), such as a common data link (CDL) protocol.

Abstract: A system includes a transmitter node and a receiver node. Each node of the transmitter node and the receiver node are time synchronized to apply Doppler corrections associated with said node's own motions relative to a stationary common inertial reference frame. The stationary common inertial reference frame is known to the transmitter node and the receiver node prior to the transmitter node transmitting a plurality of signals to the receiver node and prior to the receiver node receiving the plurality of signals from the transmitter node. The receiver node performs adaptive digitization of the signals to account for a speed of the platform.

Abstract: A system for detecting threats at an area is disclosed. The system may include a controller including one or more processors configured to execute a set of program instructions stored in a memory. The set of program instructions may be configured to cause the one or more processors to receive safe historical data of an area configured to be representative of a lack of threats, receive new data of the area from one or more nodes, compare the new data and the safe historical data to identify a difference between the new data and the safe historical data, and update a database based on the difference.

Abstract: A method is disclosed herein. The method includes receiving, by a processor, a first acceleration data from an accelerometer, calculating, by the processor, a change in velocity based on the first acceleration data, the change in velocity being calculated over a first period of time, and adjusting, by the processor, a timing sequence based on the change in velocity.

Abstract: A system may include a processor configured to: (a) obtain parameters; (b) based on the parameters, update flight-state data associated with an aircraft; (c) obtain a trained machine learning (ML) model; (d) based at least on the updated flight-state data and the trained ML model, infer a direction from a current cell for a reroute; (e) based on the inferred direction and the updated flight-state data, set the current cell and identify neighboring cells; (f) calculate an optimal next cell by using a shortest path finding (SPF) algorithm to select the optimal next cell from the neighboring cells; (g) iteratively repeat steps (d) through (f) such that the current cell is set as the optimal next cell until a goal state is reached; (h) construct a re-route using optimal cells iteratively calculated in step (f); and (i) output the re-route.

Abstract: A method is disclosed herein. The method includes determining, by a processor, a first time value in response to a switch being actuated a first time by a first striker, determining, by the processor, a second time value in response to the switch being actuated a second time by a second striker, the second striker disposed a first distance from the first striker and the second time value being after the first time value, calculating, by the processor, a change in time between the first time value and the second time value, and adjusting, by the processor, a timing sequence based on the change in time.

Abstract: A radar system identifies the presence of moderate intensity icing based on a single pulse reflectivity versus ice water content relationship. The radar then identifies convective cores in proximity to the aircraft and records features of those convective cores. Convection information, including storm tops, temperature, and cell topology, is used to indicate the presence of severe icing. A trained neural network may relate the various data to make a high intensity icing determination.

Abstract: A radar system executes an ice crystal detection method where filtered radar power returns with atmospheric ice concentration from a single beam are correlated. Filtered power returns from a typical radar pulse sequence are compared to detect high-altitude ice crystals. Individual, filtered pulses are correlated by bin.

Abstract: A system and method utilizing an existing boresighted HUD and a camera to determine the transformational and rotational relationships between the camera image and the boresighted HUD image of an aircraft to properly orient the camera for landing operations. Known boresight features are identified in a HUD image and are related to the same boresight features in a camera image, and transformations are applied to align pixels in the camera image to the pixel locations of the boresight features in the HUD image. Object recognition algorithms may be employed to identify the boresight features in the camera image.

Abstract: A system and related method for multiple-sensitivity optical phase modulation splits an optical carrier generated by a photonic source into at least two copies and directs the copies (e.g., via optical circulators or polarization rotators) to an electro-optical (EO) phase modulator such that the phase modulator phase-modulates each optical copy according to a received radio frequency (RF) signal of interest based on characteristics distinct to each optical copy (e.g., optical path direction, signal polarization) that provide for phase modulation of each optical copy at a different sensitivity voltage. The variably modified optical copies are directed to a photonic processor for further signal processing in the optical domain.

Abstract: A run-time assurance module (6) comprises a contingency planner (26) arranged to generate an initial contingency plan having an associated safety-critical decision point, where the initial contingency plan (ICP) is stored as a current contingency plan in a memory (30). The assurance module (6) receives a mission plan (MP) from a mission planner (4). When the mission plan (MP) is being carried out, the contingency planner (26) processes at least one condition input, and generates a new contingency plan (NCP) based on the condition input. When the new contingency plan (NCP) satisfies a safety criterion and the safety-critical decision point associated with the new contingency plan (NCP) will occur later in time than the safety-critical decision point associated with the current contingency plan (CCP), the new contingency plan (NCP) is stored in the memory (30) as the current contingency plan (CCP).

Abstract: An aircraft-based pilot safety system (PSS) includes cameras or other gaze sensors fixed at an aircraft pilot and configured to capture an image stream focused on the pilot's eyes. The gaze sensors continually assess the gaze direction of the pilot (e.g., toward a display, instrument panel, and/or indicator within the cockpit that the pilot is currently looking at or focusing on) and thereby can establish when the pilot is executing a scan pattern and if that scan pattern is nominal for the current flight context by comparing the scan pattern to context-specific reference scan patterns. If, for example, the pilot's gaze deviates from where it should be (e.g., as determined by the current flight segment) or the current scan pattern is interrupted, the system may prompt the pilot to redirect their gaze or resume the scan pattern.

Abstract: A shock load attenuation device is provided. The shock load attenuation device includes a crushable material; a first compartment in the crushable material surrounding a first line; and a second compartment in the crushable material surrounding a second line. In response to the first line being acted upon by a first force and the second line being acted upon by a second force, a first loop in the first line is configured to slide along the second line and a first loop in the second line is configured to slide along the first line, crushing the crushable material.